发明名称 Self-aligning roll out guidance system
摘要 Guidance along the runway centerline when visibility conditions do not permit adequate visual cues for manual control are provided utilizing lateral acceleration and bank angle information. An aircraft type airborne vehicle can touchdown with a crab angle in the presence of a crosswind and the present system provides the proper command to decrab the aircraft and return the aircraft to the centerline.
申请公布号 US4006870(A) 申请公布日期 1977.02.08
申请号 US19750594833 申请日期 1975.07.10
申请人 THE BOEING COMPANY 发明人 BOONE, JIMMIE H.;SIMPSON, ROBERT D.
分类号 G05D1/02;(IPC1-7):G05D1/12 主分类号 G05D1/02
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